• Title/Summary/Keyword: Dislocation Damping

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Internal Friction Behavior in AZ31 Magnesium Alloy after Annealing Treatment (AZ31 마그네슘 합금의 어닐링 이후 내부마찰 거동)

  • Kwak, Juho;Kang, Changyong;Kim, Kwonhoo
    • Journal of Power System Engineering
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    • v.22 no.1
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    • pp.87-93
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    • 2018
  • Specimens were machined out from hot-rolled AZ31 magnesium alloy, and deformed at 623K with rolling reduction of 30%. After hot rolling, specimens were annealed at various range of temperature and time. In this study, static recrystallization was occurred during heat treatment, however, variation of main component and intensity of texture was not revealed. The results of microstructure observation, damping capacity test and dislocation mechanism indicated that increasing of damping capacity was caused by grain growth. It means that grain size is effective factor to damping capacity.

Damping Capacities of Nonthermoelastic BCC and HCP Martensites of Fe-Mn Binary System (Fe-Mn 이원계에서 비열탄성형 BCC 마르텐사이트와 HCP 마르텐사이트의 진동감쇠능)

  • Choi, C.S.;Kim, J.D.;Moon, I.G.;Baik, S.H.
    • Journal of the Korean Society for Heat Treatment
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    • v.4 no.4
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    • pp.15-23
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    • 1991
  • The damping capacities of the nonthermoelastic bcc type lath martensite and of the nonthermoelastic hcp type thin plate martensite in Fe-Mn alloys were studied. Fe-17%Mn alloy showing the hcp type thin plate martensite was superior to Fe-4%Mn alloy having the bcc type lath martensite in damping capacity. The damping capacity of the Fe-17%Mn alloy became greater with increasing the hcp martensite volume fraction. The damping mechanism of the Fe-4%Mn alloy was well explained by the dislocation model. However, the damping mechanism of the Fe-17%Mn alloy was explained on the basis of austenite/martensite interface moving model. The two alloys showed almost same levels of tensile strength. However, the elongation was greater in the Fe-17%Mn alloy than in the Fe-4%Mn alloy, showing lower yield strength in the former than in the latter. This result was considered to be attributed to formation of stress-induced martensite during tension test.

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Effect of Solution-Treatment Temperature on Microstructure and Damping Capacity of a Martensitic Fe-7%Ni-0.4%C Alloy (Fe-7%Ni-0.4%C 마르텐사이트합금의 미세조직과 진동감쇠능에 미치는 용체화처리온도의 영향)

  • Lee, Young-Kook;Jee, Kwang-Koo;Choi, Chong-Sool
    • Journal of the Korean Society for Heat Treatment
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    • v.11 no.1
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    • pp.1-9
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    • 1998
  • The objective of this study is to investigate the effect of solution-treatment temperature on the microstructure and damping capacity of a martensitic Fe-7%Ni-0.4%C alloy. The size of lath increased from $0.3{\mu}m$ to $0.55{\mu}m$ with increasing the solution-treatment temperature from 700 to $1100^{\circ}C$. In addition, the size of block, packet, and austenite grain had tendency to increase with increasing solution-treatment temperature. The damping capacity of the Fe-7%Ni-0.4%C martensitic alloy decreased with increasing the solution treatment temperature. The reason is not attributed to the increase in the size of lath, block, packet, and austenite grain, but to the increase in vacancy concentration which hinders dislocation motion.

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High Temperature Creep Strength of Mg-Nd-Zr-Zn Alloy in Sand Castings (사형주조한 Mg-Nd-Zr-Zn합금의 고온 크리이프강도)

  • Kang, Dae-Min;Park, Kyung-Do;Park, Ji-Hee
    • Journal of the Korean Society of Manufacturing Process Engineers
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    • v.10 no.6
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    • pp.83-88
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    • 2011
  • Magnesium alloys have been focussed for the applications for lightweight of vehicle and electronics due to their high strength, low specific density and good damping capacity. This paper deals with the creep strength of Mg-Nd-Zr-Zn alloy. For the alloy, pure magnesium(99.9%) was melt with atmosphere of $0.3%SF_6$ and $25%CO_2$. After melting, 0.3% of zinc was inserted to stir for 10min at elevated temperature of $770^{\circ}C$. Master alloys of Mg-15%Nd and Mg-15%Zr were stirred in furnace. The creep tests were performed to obtain creep rate and rupture in the temperature range of 200 to $220^{\circ}C$ and 280 to $310^{\circ}C$ at an applied stress of 156 to 172MPa and 78 to 94MPa, respectively. The deformation mechanism was predicted dislocation climb from measured apparent activation energy and stress exponent. Also the increaser the temperature and stress the lower the stress exponent and activation energy. Finally, LMP parameter gives good information for the predicted creep rupture life.